Automatic Three-Point Landing of a UAV with H∞-Controlin D-Implementation

被引：5

作者：

Sedlmair, Nicolas ^{[1
]}

Theis, Julian ^{[1
]}

Thielecke, Frank ^{[1
]}

机构：

[1] Hamburg Univ Technol, Inst Aircraft Syst Engn, Hamburg, Germany

来源：

IFAC PAPERSONLINE | 2019年 / 52卷 / 12期

关键词：

flight control; robust control applications; multivariable control systems; AUTOLAND CONTROLLER; AUTOPILOT DESIGN; AIRCRAFT;

D O I：

10.1016/j.ifacol.2019.11.262

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

A multivariable flight control law for automatic landing of an unmanned aircraft with tailwheel gear configuration is developed in this paper. The control law is obtained using H-infinity-synthesis and implemented in a differential form to facilitate bumpless transfer, i.e. correct initialization when switching control laws, and anti-windup compensation. The controller is evaluated using a validated high-fidelity model of the aircraft and Monte-Carlo simulations. Copyright (C) 2019. The Authors. Published by Elsevier Ltd. All rights reserved.

引用

页码：316 / 321

页数：6

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